Observer Based Optimal Vibration Control of a Full Aircraft System Having Active Landing Gears and Biodynamic Pilot Model

Table 4

Comparison of peak values of landing gear suspension stroke and tire deflection responses for both controlled and uncontrolled cases.

	Bump			Random
	Passive	Controller 2	Controller 1	Passive	Controller 2	Controller 1
	0.0857	0.0469	0.0471	0.0151	0.0083	0.0078
	0.1250	0.1256	0.1436	0.0101	0.0087	0.0091
	0.0850	0.0741	0.0849	0.0105	0.0053	0.0058
	0.0033	0.0007	0.0008	0.0041	0.0028	0.0027
	0.0100	0.0045	0.0041	0.0055	0.0037	0.0031
	0.0093	0.0027	0.0024	0.0053	0.0032	0.0028